View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20804U 90083A 25013.01453976 .00000074 00000-0 61897-4 0 9996
2 20804 82.9388 193.0246 0035681 288.8232 229.7145 13.74503341722030
| Epoch (UTC): | 13 January 2025 00:20:56 |
| Eccentricity: | 0.0035681 |
| inclination: | 82.9388° |
| perigee height: | 957 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 193.0246° |
| argument of perigee: | 288.8232° |
| revolutions per day: | 13.74503341 |
| mean anomaly at epoch: | 229.7145° |
| orbit number at epoch: | 72203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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